TRANS - Training Guide Flashcards
- What if not installed properly can result in
loss of cabin pressure in flight?
TO 1T-1A-1 (2-3)
Escape Hatch
- What is required before changing any
electrical source?
TO 1T-1A-1 (2-4)
Advise the crew
- What is required whenever power is applied to the aircraft?
TO 1T-1A-1 (2-4)
One crewmember must be onboard at all times
- Failure to check all eight door locking pins
showing white can result in what?
TO 1T-1A-1 (2-10)
Door opening inflight
- When are you required to have seatbelts
adjusted and fastened?
TO 1T-1A-1 (2-11)
While performing pilot/copilot duties and the aircraft is in motion
- Where should the operating engine’s throttle be for a generator assisted start of the second engine and why?
TO 1T-1A-1 (5-7)
Must be at IDLE
- What are the minimum voltage requirements for battery start of an engine? A
GPU start?
TO 1T-1A-1 (2-14)
Battery: 22 V
GPU: 28 V
- What are you required to do if any
abnormal start indications occur prior to
moving the associated throttle out of
CUTOFF into IDLE?
TO 1T-1A-1 (2-15)
Starter switch DISENGAGE
- During engine start, after placing the
throttle to IDLE you experience a
malfunction. What do you do? What is the starter ops limit and does it apply in this case?
TO 1T-1A-1 (2-15, 5-7)
Place the throttle in CUTOFF, Ignition switch OFF, let the starter purge fuel for 15 sec
Ops Limits:
30 sec > 5 minutes
30 sec > 15 minutes
30 sec > 60 minutes
- During a battery start, when do you place the
start selector to OFF? Why?
TO 1T-1A-1 (2-15)
Wait until engine has stabilized at idle.
Allows generator to reach full operating capacity
- When does the stick shaker activate during the Master Test System check of the stall warning system? Why does it activate twice at different AOAs?
TO 1T-1A-1 (2-16)
0.4 - 0.5, 0.7
Testing of the altitude compensator
- What do you do if an anti-skid
malfunction occurs with an associated loss
of brakes? What if braking is not restored?
TO 1T-1A-1 (2-19)
Anti-skid OFF, try braking from both sides.
If not restored use emergency brakes
- When should the anti-skid not be tested? How long will normal braking be
unavailable after performing the test?
TO 1T-1A-1 (2-19)
Do not test in CONGESTED areas
4 secs
- When must fuel crossfeed not be used? Why?
TO 1T-1A-1 (2-19)
Takeoff, Final Approach, Landing
Prevents dual engine flameout
- What must be briefed during the crew
briefing before taking off?
TO 1T-1A-1 (2-21,22)
- Normal T/O
- Emergency T/O and return
- Departure procedures
- Altimeter setting
- Altitude preselect
- What is paramount that crewmembers are
briefed on prior to flight?
TO 1T-1A-1 (2-22)
Crewmember’s respective actions and responsibilities during flight ops
- The crew member occupying the jump seat
will never do what?
TO 1T-1A-1 (4-1)
Never actuate:
- flights controls
- configuration controls
- controls on shroud panel/instrument panel
- Pilots shall not exchange seat when?
TO 1T-1A-1 (4-2)
If there are only two pilots aboard
- All crew members will monitor UHF or
VHF ATC communications in addition to
interphone when?
TO 1T-1A-1 (4-3)
T/O
Descent
Landing
- What is the standard for Publications / Equipment / Special Clothing Requirements? What at a minimum must out of the pubs kit and readily available?
3 FTS OI, A3.1.27
Required flight crew
publications/equipment will be IAW AFI 11-2T-1V3.
Ensure DoD FLIP is current and contains coverage
for route of flight and potential divert options.
Clothing requirements will be IAW AFI 11-2T-
1V3_71OGSUP.
At a minimum, applicable enroute IFR/VFR charts, and approach plates will be out of the
pubs kit and readily accessible to the PF and PM.
- What specific publications, charts, and equipment does the AFI 11-2T-1V3 and the OG Sup to the Vol 3 require?
AFI 11-2T-1V3, 3.1.2
- Dash-1
- Dash-1-1
- Green Crew checklist
- Fanfold checklist
- Flight gloves
- Suitable terrain charts
- Life raft and life preservers if over water
- What is the standard for clearing?
3 FTS OI, A3.1.4
PF will fly the aircraft and may attempt to locate the target without sacrificing aircraft
control. PNF will note target clock-position and high/low and if it is a factor to the aircraft. If a jump seat
is on board, he/she will notify the crew when aircraft safety is in jeopardy by actively searching for traffic
while monitoring the TCAS display. Clearing on the radios will be accomplished by all crew members.
- What is the standard for Radio Procedures and Discipline?
3 FTS OI, A3.1.5
PNF will handle ATC radios to the maximum extent possible.
- How is the transfer of aircraft control accomplished while handflying? On autopilot? With inoperative intercom? (i.e. what is the standard for Transfer of Aircraft Control?)
3 FTS OI, 3.1.6, AFMAN11-247, 1.7
Handflying: “(Co)pilot you have the aircraft”
Autopilot: Ensure positive verbal transfer of who has the A/C and which flight director is controlling.
Intercom Inop: Shake to take/Push to pass. Show hands up once passed
- What is the standard for Simulated EPs?
3 FTS OI, A3.1.28
All simulated EPs will be executed IAW AFI 11-2T-1V3 and
this instruction with the IP introducing all EPs as “simulated.”
- What restrictions does the 11-2T-1V3 place on simulated EPs?
AFI 11-2T-1V3, 3.15
Min Wx: 1,500 and 3
Do not practice simulated T/O, approach, or Ldg unless IP is sitting up front.
No SE go-around with 30 flaps
- Brief all airborne simulated emergencies prior to execution. Compound or multiple simulated emergencies are prohibited.
- Maintain clear of clouds when conducting simulated emergencies.
- Do not initiate practice simulated engine failure below 500 feet AGL during takeoff or landing.
- Do not fly VFR single-engine and no-flap patterns from the tactical pattern.
- Discontinue simulated emergencies if intracockpit communications cannot be maintained.
- How is weight and balance calculated if 3 or less crew members are on board? What if there are more than 3 crew members? (i.e. what is the standard for Weight and Balance?)
3 FTS OI, A3.1.28 and 4.1.3.12
Canned Form F at step desk.
If more than 3, coordinate with SUP.
- What is the standard for Crew Duties (L/R)?
3 FTS OI, A3.1.13
Person performing the walk-around should also perform step “2. Cargo/passenger compartment (W) - Checked”
The pilot in the left seat will engage the autopilot while the pilot in the right seat checks their respective switches during step “17. Autopilot –
Checked/DISENGAGED” of the BEFORE EXTERIOR INSPECTION.
- What is the standard for Delays / Spares?
3 FTS OI, A3.1.14
Contact Liberty Ops
New weight and balance in black binder near jump
- What is the standard for Avionics Set-up?
3 FTS OI, A3.1.16
Abv/Blo, Relative, 10nm, TA/RA and test
Once PF flying acknowledges HDG or ALT, PM will set appropriate instrument
- What is the standard for Bird Strike?
3 FTS OI, A3.1.25
- If on final > Land
- Prior to S1 > abort
- Once airborne > leave configuration, controllabilty check
- Into engine > land as soon as possible
- At what weight is an aircraft classified as
“heavy”? What must be done if you are taking off or landing behind a “large” or “heavy” aircraft/Boeing 757? Is there any way to mitigate this?
GP (2-3), TO 1T-1A-1 (2-22, 2-30)
- Heavy = capable of T/O greater than 300,000 lbs
- 2 minutes after large A/C or helos
- 3 minutes behind 757 or heavy A/C
- T/O prior to their rotation
- Land after their touchdown
- Xwinds more than 5 knots may reduce interval
- What format do we write the date in on the DD Form 1801 (item 18 (DOF/))
GP 4-28
Enter six-digit Date/Time group to indicate
UCT filing time of flight plan. The first two digits will show date of
month. The last four digits will show the time. Example: 211145
- How would you write 330KIAS on a DD Form 1801? Mach .78 (item 15)?
GP 4-25
N0330
M078
- How would you write 9000 MSL on a DD Form 1801? FL200 (item 15)?
GP 4-25
A090
F200
- The route of flight on the 1801 flight plan must contain at least one waypoint or NAVAID within the first ______ miles of each ARTCC.
GP 4-25
200 nm (or 30 minutes flying time)
- What are the FLIGHT RULES options on the DD Form 1801 (item 8)?
GP 4-22
I - If IFR Y - If IFR then VFR V - If VFR Z - If VFR then IFR If Y or Z is entered, specify in Item 15 where the Change of Flight Rules is planned.
- What are the wake turbulence categories and definitions on the DD Form 1801 (item 9)? What do we use for the T-1?
GP 4-23
H – Heavy – >300,000 lbs Max Gross Takeoff Weight
M – Medium – 15,501 – 299,999 lbs Max Gross Takeoff Weight
L – Light – 15,500 lbs or less Max Gross Takeoff Weight
T-1 uses category M
- How would you file the Anthony Two departure out of Vance on an 1801? MOTZA 7 arrival into KAFW?
JHK2
MOTZA7
No spaces, or periods
- When is an airspeed change required? How would you file the altitude and airspeed change from the Vance MOAs to Wichita via the standard routing?
GP 4-26
Cruising speed change of 5% TAS or .01 MACH (or greater)
Example: END286044/N0315A130 DCT ANY V12 ICT
- The hydraulic power supply system
supplies hydraulic pressure to operate
what?
TO 1T-1A-1 (1-68)
Memory device: FLAPS F – L – A – P – S –
Flaps
Gear
Brakes (Speed)
Brakes (Wheel)
- How many hydraulic pumps does the
T-1A have, and what drives them? How many pumps are required to power the hydraulic system?
TO 1T-1A-1 (1-68, 1-71)
2 pumps (engine-driven variable displacement pumps)
1 pump can drive the whole system
- Each hydraulic pump supplies what rate
and psi of hydraulic fluid to it components?
TO 1T-1A-1 (1-71)
0 gpm at 1500 psi and 3.9 gpm at 1400 psi
- The hydraulic reservoir’s capacity is? What PSI does it maintain?
TO 1T-1A-1 (1-71)
1.2 gal
15 psi bleed air
- What are the hydraulic fluid shutoff
valves and how are the actuated.
TO 1T-1A-1 (1-71, 1-77)
H/F VALVE SWITCH
Fire push lights
- What is normal hydraulic pressure? What pressure does the relief valve open? What pressure indicates failure of the relief valve? What should the pilot do if this happens?
TO 1T-1A-1 (1-71)
1350 - 1550 psi, usually stabalizes at 1500
Pressure relief open at 1650
1850, then by HYD bypass switch
- When do the two hydraulic low pressure
caution annunciators illuminate? What are the indicators labeled?
TO 1T-1A-1 (1-77)
< 750 psi
- When does the low hydraulic fluid level
caution annunciator illuminate? What are the indicators labeled?
TO 1T-1A-1 (1-77)
< 0.6 gal
HYD LVL LO
- What can you expect in the event a
hydraulic line were to rupture? Why?
TO 1T-1A-1 (1-71)
Complete loss of hydraulic fluid
- How many hydraulic fluid filters are there? What happens if one gets clogged? Is there a way for the pilot to know one has been clogged?
TO 1T-1A-1 (1-71)
3, one after each pump and one for the reservoir.
No indication to pilot
- Does emergency extending your landing
gear relieve all pressure in the hydraulic
system? What closes the main landing gear doors? How many applications of the emergency brake are available after closing the main doors?
TO 1T-1A-1 (1-80, 1-93, 1-94)
No
They system uses Nitrogen pressure
7-9
- How long does normal retraction and extension of the gear take? Emergency extension?
TO 1T-1A-1 1-85, 3-42
7 sec
30 sec
- If a flap or landing gear limitation is
exceeded, the aircraft commander should
suspect damage and not do what?
TO 1T-1A-1 (5-1)
Dont change configuration unless necessary for safety of flight
- During normal operations, how does fuel flow from the tanks to the engines?
TO 1T-1A-1 (1-41, 1-45, 1-48)
Fuel gravity feeds from the aft cabin tank to the aft fuselage tank into the mid tanks.
Two electric transfer pumps move fuel from the mids to the wing tanks.
Six flapper valves in each wing allow fuel to gravity feed from the outboard to the center to the inboard bays but prevent fuel from flowing outboard.
The fuel feed chambers receive fuel from their respective inboard bays via gravity, an aft transfer jet pump (receives motive flow from the primary jet pump), and a forward jet pump (receives motive flow whenever the boost pump is on).
Each fuel feed chamber provides fuel to its respective engine through the primary jet pump, which receives motive flow from the engine driven fuel pump (with the electric boost pump as required to maintain pressure).
- What pressure differential is required for
the fuel filter bypass valve to open? What is the indication in the cockpit? What does this indicate?
TO 1T-1A-1 (1-49)
2.3 ±0.2 psi
- What is the volume of fuel in the wing
tanks under pressure refueling? Gravity
refueling? How much fuel is available in the wing tanks? Why is this important to know?
TO 1T-1A-1 (2-22)
Pressure—409 gal, gravity—423 gal
- What is the capacity of the fuel feed
chamber?
TO 1T-1A-1 (1-51)
~ 20 gal
- What are the three general types of fuel pumps are used in the T-1A? How many of each, what powers them, and where are they located?
TO 1T-1A-1 (1-41, 1-42, 1-44)
Jet pumps
electric pumps for boost and transfer
engine driven pumps
- What are the four purposes of the boost
pumps?
TO 1T-1A-1 (1-41, 42)
- Engine starting
- Backup for primary jet pumps
- Source of pressure for transfer jet pumps
- Crossfeed
- When do the boost pumps automatically
come on? In which cases must the boost pumps be reset?
TO 1T-1A-1 (1-42)
Fuel feed line pressure < 5 psi, fuel feed drops below approx. 11 gal, engine starting, crossfeed
- When do the transfer pumps come on?
What must be operating for the transfer
pumps to be on?
TO 1T-1A-1 (1-42)
Whenever there is fuel in mid tanks and an operating generator
- What are check valves used for in the
fuel system?
TO 1T-1A-1 (1-45)
Prevents backflow of fuel
- What causes the transfer pumps to turn off?
TO 1T-1A-1 (1-42, 1-49)
In automatic mode, as fuel is exhausted in either mid tank, a combination of a float switch and the pressure going below 5.0±0.5 psi causes the transfer pump to automatically shut off.
- At what pressure does wing tank
overpressure annunciator illuminate? What is the problem? What immediate action should be taken in flight?
TO 1T-1A-1 (1-49, 3-17, 3-54)
Wing overpressure is annunciated at 3.5±0.5 psi with an amber legend, L or R WG TK OV PRESS. A wing tank overpressure condition indicates a malfunction of the wing fuel level control pilot valves, which in normal operation closes the shutoff valve to stop fuel flow. If in a climb or descent, maintain level flight.
- When does the fuel feed level low light
annunciator illuminate?
TO 1T-1A-1 (1-49, 1-51, 3-18, 3-54)
A float switch closes the respective annunciator circuit when approximately 70 pounds (11 gallons) of usable fuel remains in the fuel feed chamber.
- When does the L or R FUEL LEVEL LO light illuminate?
TO 1T-1A-1 (1-50, 3-18, 3-54)
When the respective wing tank has 200 pounds (32 gallons) or less of useable fuel.
- When are the fuel level indicators
unreliable? What happens if the indicator system fails? Why?
TO 1T-1A-1 (1-50)
(N) Fuel quantity indicators are unreliable at high angles of attack and/or any angles of side-slip. In the event of indicator system failure, both
gages’ dial pointers move off-scale to below the
zero mark to indicate an inoperative condition.
The separate pointer position for an inoperative
gage prevents misinterpretation of very low or
out-of-fuel indications.
- Will cross feeding supply fuel to both
engines simultaneously?
TO 1T-1A-1 (1-48) T
TO 1T-1A-1 (5-11)
Yes
- What type of power system is the primary
source of power for the T-1A? How does the AC system receive power?
TO 1T-1A-1 (1- 53)
The dc power system is the primary source of power for most aircraft systems. It is also the power source for the inverters used in the ac power system.
- What type and how much power does
each generator supply?
TO 1T-1A-1 (1-53 )
The generators supply primary 28 VDC power for the dc power system.
- At what % N2 does the generator start
acting like a generator?
TO1T-1A-1 (1-25)
35-40% N2 the starter/generator begins to operate as a generator
- When the power leaves the generator
where does it go?
TO 1T-1A-1 (1-53)
Power is distributed from each generator to
its respective LH and RH main bus, then to the LH and RH load bus. The main buses are paralleled through the LH BUS TIE and RH BUS TIE circuit breakers and supply power to the battery charge bus.
- What type of battery does the T-1A have? Where is it located?
TO 1T-1A-1 (1-53)
24-volt, 40-ampere-hour lead-acid battery, located in the aft fuselage compartment,
- What are the three purposes of the battery?
TO 1T-1A-1 (1-53)
It supplies secondary electrical power for ground operation, engine starting, and emergency
requirements.
- What is the sole purpose of the battery
feeder protection unit?
TO 1T-1A-1 (1-53)
The battery feeder protection unit detects a ground fault that may occur in the battery and external power feeder and ground lines.
- What is external DC power used for?
TO 1T-1A-1 (1- 58)
External dc power is used for ground engine starts, battery charging, and maintenance requiring electrical power.
blower and/or windshield heat at the same time as using electric heat with external ground power?
TO 1T-1A-1 (1-58)
Operating these systems in combination while using the GPU causes an excessive amperage pull which could result in overheating the ground plug and receptacle.
- What provides ground fault protection?
TO 1T-1A-1 (1-58)
(N) Ground fault protection is provided by the
battery protection circuits.
- What are some items on the standby bus? Where is the standby battery located?
TO 1T-1A-1 (1-58)
The standby battery is located in the nose electronics compartment and supplies Standby Bus Power to (memory aid: CRUISSE): • Copilot instrument lights • RTU #1 • UHF radio • No. 1 ITT indicator • Standby attitude indicator • Standby altimeter vibrator • Electronic fuel control - start
- What is the purpose of the AHRS
battery? Where is it located?
TO 1T-1A-1 (1-58)
The AHRS auxiliary battery, mounted in the avionics rack, provides power to either/or both AHRS computers if either the left load bus and/or right load bus power fails.
- What keeps the standby battery charged?
TO 1T-1A-1 (1-63)
The emergency bus supplies a charge current to the standby battery.
- What are some key items that are located on the Emergency Bus? (memory aid: SLEEVES)
TO 1T-1A-1 (1-62)
SLEEVES • Select LH Engine Instruments (N1, N2) • Landing Gear Position Indicators • Emergency Pitch Trim and warning • Emergency Smoke/Fire Detect & Extinguish (fire bell only not warning lights) • VHF Navigation Radio #1 • Engine ignition and control (left engine) • Standby Bus Also, other good stuff Batt FDR Prot (Batt Cutoff) Flood Instruments Wing Anti-Ice System 1
